FR2889264B1 - Verrouillage des aubes dans un rotor de soufflante - Google Patents

Verrouillage des aubes dans un rotor de soufflante

Info

Publication number
FR2889264B1
FR2889264B1 FR0508121A FR0508121A FR2889264B1 FR 2889264 B1 FR2889264 B1 FR 2889264B1 FR 0508121 A FR0508121 A FR 0508121A FR 0508121 A FR0508121 A FR 0508121A FR 2889264 B1 FR2889264 B1 FR 2889264B1
Authority
FR
France
Prior art keywords
aubes
locking
blower rotor
blower
rotor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR0508121A
Other languages
English (en)
Other versions
FR2889264A1 (fr
Inventor
Herve Marc Philippe Buisson
Jean Luc Goga
Eric Lefebvre
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR0508121A priority Critical patent/FR2889264B1/fr
Priority to CA2554092A priority patent/CA2554092C/fr
Priority to EP06118048.5A priority patent/EP1748154B1/fr
Priority to US11/494,582 priority patent/US7686585B2/en
Priority to RU2006127495/06A priority patent/RU2396470C2/ru
Publication of FR2889264A1 publication Critical patent/FR2889264A1/fr
Application granted granted Critical
Publication of FR2889264B1 publication Critical patent/FR2889264B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/322—Blade mountings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/32—Locking, e.g. by final locking blades or keys
    • F01D5/326—Locking of axial insertion type blades by other means
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0508121A 2005-07-29 2005-07-29 Verrouillage des aubes dans un rotor de soufflante Active FR2889264B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR0508121A FR2889264B1 (fr) 2005-07-29 2005-07-29 Verrouillage des aubes dans un rotor de soufflante
CA2554092A CA2554092C (fr) 2005-07-29 2006-07-26 Verrouillage des aubes dans un rotor de soufflante
EP06118048.5A EP1748154B1 (fr) 2005-07-29 2006-07-28 Verrouillage des aubes dans un rotor de soufflante
US11/494,582 US7686585B2 (en) 2005-07-29 2006-07-28 Locking of the blades in a fan rotor
RU2006127495/06A RU2396470C2 (ru) 2005-07-29 2006-07-28 Ротор вентилятора турбореактивного двигателя, вентилятор и авиационный турбореактивный двигатель

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0508121A FR2889264B1 (fr) 2005-07-29 2005-07-29 Verrouillage des aubes dans un rotor de soufflante

Publications (2)

Publication Number Publication Date
FR2889264A1 FR2889264A1 (fr) 2007-02-02
FR2889264B1 true FR2889264B1 (fr) 2007-11-02

Family

ID=36371048

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0508121A Active FR2889264B1 (fr) 2005-07-29 2005-07-29 Verrouillage des aubes dans un rotor de soufflante

Country Status (5)

Country Link
US (1) US7686585B2 (fr)
EP (1) EP1748154B1 (fr)
CA (1) CA2554092C (fr)
FR (1) FR2889264B1 (fr)
RU (1) RU2396470C2 (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2945329B1 (fr) * 2009-05-06 2011-06-03 Snecma Rotor de soufflante d'un turboracteur d'avion
JP5561461B2 (ja) * 2009-06-09 2014-07-30 株式会社Ｉｈｉ 動翼保持構造
FR2974864B1 (fr) * 2011-05-04 2016-05-27 Snecma Rotor de turbomachine avec moyen de retenue axiale des aubes
US10072509B2 (en) 2013-03-06 2018-09-11 United Technologies Corporation Gas turbine engine nose cone attachment
GB201317161D0 (en) 2013-09-27 2013-11-06 Rolls Royce Plc Retainer plate
GB201318623D0 (en) 2013-10-22 2013-12-04 Rolls Royce Plc Retainer plate
US11220920B2 (en) 2014-04-07 2022-01-11 Safran Aircraft Engines Turbine engine rotor lock
KR102182102B1 (ko) * 2014-11-27 2020-11-23 한화에어로스페이스 주식회사 터빈 장치
CN104500446A (zh) * 2014-12-14 2015-04-08 惠阳航空螺旋桨有限责任公司 风洞轴流压缩机转子复合材料叶片根部连接结构
US10400784B2 (en) * 2015-05-27 2019-09-03 United Technologies Corporation Fan blade attachment root with improved strain response
FR3057908B1 (fr) * 2016-10-21 2019-11-22 Safran Aircraft Engines Ensemble rotatif d'une turbomachine muni d'un systeme de maintien axial d'une aube
US10393135B2 (en) 2017-02-09 2019-08-27 DOOSAN Heavy Industries Construction Co., LTD Compressor blade locking mechanism in disk with axial groove
FR3092861B1 (fr) * 2019-02-18 2023-02-10 Safran Aircraft Engines Ensemble de turbomachine comportant un taquet sur un jonc d'etancheite

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1332988A (fr) * 1961-10-18 1963-07-19 Daimler Benz Ag Dispositif d'assujettissement pour aubes de machines à écoulement ou circulation de fluide
US4033705A (en) * 1976-04-26 1977-07-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Blade retainer assembly
US4265595A (en) * 1979-01-02 1981-05-05 General Electric Company Turbomachinery blade retaining assembly
FR2502690B1 (fr) * 1981-03-27 1985-09-13 Snecma Dispositif de verrouillage d'aubes de soufflante et de fixation de capot avant d'un turboreacteur
FR2535794A1 (fr) * 1982-11-08 1984-05-11 Snecma Dispositif de retenue axiale et radiale d'aubes de soufflante
US5123813A (en) * 1991-03-01 1992-06-23 General Electric Company Apparatus for preloading an airfoil blade in a gas turbine engine
US5259728A (en) * 1992-05-08 1993-11-09 General Electric Company Bladed disk assembly
US5350279A (en) * 1993-07-02 1994-09-27 General Electric Company Gas turbine engine blade retainer sub-assembly
US6457942B1 (en) * 2000-11-27 2002-10-01 General Electric Company Fan blade retainer

Also Published As

Publication number Publication date
RU2396470C2 (ru) 2010-08-10
EP1748154A2 (fr) 2007-01-31
RU2006127495A (ru) 2008-02-10
CA2554092C (fr) 2013-12-10
FR2889264A1 (fr) 2007-02-02
US20090226321A1 (en) 2009-09-10
US7686585B2 (en) 2010-03-30
EP1748154A3 (fr) 2012-10-24
EP1748154B1 (fr) 2016-01-13
CA2554092A1 (fr) 2007-01-29

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